SIMILTUDE LAWS FOR A FLOW OF GAS IN A THIN HYPERSONIC NOZZLE,

Abstract

A similitude law for flow of gas in a hypersonic nozzle taking into account the interactions of the boundary layer with a potential nucleus similar to a previously established similitude law for external flow past thin bodies is obtained. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 26, 1965
Accession Number
AD0625787

Entities

People

  • Yu. L. Zhilin

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundaries
  • Boundary Layer
  • Hypersonic Nozzles
  • Layers
  • Nozzles

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow